20031008025619I

Incident · Minor damage

FAA incident report · Piper PA-24-250 · Westfield, MA · October 8, 2003

Date
October 8, 2003 · 20:43 local
Place
Westfield, MA
Airport
Barnes Municipal
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N7621E
Reported as
Piper PA24250
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,450 total150 in this make and model60 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Aircraft landed runway 20 at Westfield, MA, at 8:43 pm local time. On rollout, the right main and nose landing gear collapsed. The pilot stated that the landing gear position light was green and the selector was down. No aural warning was heard. Investigation of the retraction system with the aircraft on jacks revealed that the gear retraction tube inboard arm had fractured. This arm connects the right main and nose gear push pull cables to the retract mechanism. A visual inspection of the fracture surfaces indicated a portion of the fracture may have occurred prior to this incident.

As the FAA filed it

(-23) AIRCRAFT LANDED RUNWAY 20 AT WESTFIELD, MA, AT 8:43 PM LOCAL TIME. ON ROLLOUT, THE RIGHT MAIN AND NOSE LANDING GEAR COLLAPSED. THE PILOT STATED THAT THE LANDING GEAR POSITION LIGHT WAS GREEN AND THE SELECTOR WAS DOWN. NO AURAL WARNING WAS HEARD. INVESTIGATION OF THE RETRACTION SYSTEM WITH THE AIRCRAFT ON JACKS REVEALED THAT THE GEAR RETRACTION TUBE INBOARD ARM HAD FRACTURED. THIS ARM CONNECTS THE RIGHT MAIN AND NOSE GEAR PUSH PULL CABLES TO THE RETRACT MECHANISM. A VISUAL INSPECTION OF THE FRACTURE SURFACES INDICATED A PORTION OF THE FRACTURE MAY HAVE OCCURRED PRIOR TO THIS INCIDENT.

Other reports on N7621E · 1

Matched to the same aircraft by N-number and date.